View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 60304U 26145.22140331 +.00000000 +00000-0 +32271-4 0 00009
2 60304 53.1586 128.9964 0001141 98.1880 261.9268 15.69672421 00
| Epoch (UTC): | 25 May 2026 05:18:49 |
| Eccentricity: | 0.0001141 |
| inclination: | 53.1586° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 128.9964° |
| argument of perigee: | 98.1880° |
| revolutions per day: | 15.69672421 |
| mean anomaly at epoch: | 261.9268° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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